EP4130332A3 - Revêtement de barrière thermique résistant à l'éclatement - Google Patents

Revêtement de barrière thermique résistant à l'éclatement Download PDF

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Publication number
EP4130332A3
EP4130332A3 EP22181358.7A EP22181358A EP4130332A3 EP 4130332 A3 EP4130332 A3 EP 4130332A3 EP 22181358 A EP22181358 A EP 22181358A EP 4130332 A3 EP4130332 A3 EP 4130332A3
Authority
EP
European Patent Office
Prior art keywords
cathode
layer
barrier coating
thermal barrier
deposition
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP22181358.7A
Other languages
German (de)
English (en)
Other versions
EP4130332A2 (fr
Inventor
Mladen F. Trubelja
Dinesh K. Gupta
Brian S. Tryon
Mark T. Ucasz
Benjamin J. ZIMMERMANN
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RTX Corp
Original Assignee
Raytheon Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=51528406&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP4130332(A3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Raytheon Technologies Corp filed Critical Raytheon Technologies Corp
Publication of EP4130332A2 publication Critical patent/EP4130332A2/fr
Publication of EP4130332A3 publication Critical patent/EP4130332A3/fr
Pending legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/08—Oxides
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14—Metallic material, boron or silicon
    • C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24—Vacuum evaporation
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
    • C23C14/24—Vacuum evaporation
    • C23C14/32—Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
    • C23C14/325—Electric arc evaporation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/175—Superalloys
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • F05D2300/2118—Zirconium oxides
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12611—Oxide-containing component
    • Y10T428/12618—Plural oxides

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Physical Vapour Deposition (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Analytical Chemistry (AREA)
EP22181358.7A 2013-03-15 2014-03-13 Revêtement de barrière thermique résistant à l'éclatement Pending EP4130332A3 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US201361800594P 2013-03-15 2013-03-15
EP14767987.2A EP2971239B1 (fr) 2013-03-15 2014-03-13 Revêtement formant barrière thermique et résistant à la spallation
EP18166188.5A EP3372707B1 (fr) 2013-03-15 2014-03-13 Revêtement de barrière thermique résistant à l'éclatement
PCT/US2014/026452 WO2014151788A1 (fr) 2013-03-15 2014-03-13 Revêtement formant barrière thermique et résistant à la spallation

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
EP14767987.2A Division EP2971239B1 (fr) 2013-03-15 2014-03-13 Revêtement formant barrière thermique et résistant à la spallation
EP18166188.5A Division EP3372707B1 (fr) 2013-03-15 2014-03-13 Revêtement de barrière thermique résistant à l'éclatement

Publications (2)

Publication Number Publication Date
EP4130332A2 EP4130332A2 (fr) 2023-02-08
EP4130332A3 true EP4130332A3 (fr) 2023-05-31

Family

ID=51528406

Family Applications (3)

Application Number Title Priority Date Filing Date
EP18166188.5A Active EP3372707B1 (fr) 2013-03-15 2014-03-13 Revêtement de barrière thermique résistant à l'éclatement
EP14767987.2A Active EP2971239B1 (fr) 2013-03-15 2014-03-13 Revêtement formant barrière thermique et résistant à la spallation
EP22181358.7A Pending EP4130332A3 (fr) 2013-03-15 2014-03-13 Revêtement de barrière thermique résistant à l'éclatement

Family Applications Before (2)

Application Number Title Priority Date Filing Date
EP18166188.5A Active EP3372707B1 (fr) 2013-03-15 2014-03-13 Revêtement de barrière thermique résistant à l'éclatement
EP14767987.2A Active EP2971239B1 (fr) 2013-03-15 2014-03-13 Revêtement formant barrière thermique et résistant à la spallation

Country Status (3)

Country Link
US (2) US9506140B2 (fr)
EP (3) EP3372707B1 (fr)
WO (1) WO2014151788A1 (fr)

Families Citing this family (9)

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US10364490B2 (en) * 2013-12-10 2019-07-30 United Technologies Corporation Chromizing over cathodic arc coating
US9834835B2 (en) * 2015-02-18 2017-12-05 United Technologies Corporation Fire containment coating system for titanium
US10436042B2 (en) 2015-12-01 2019-10-08 United Technologies Corporation Thermal barrier coatings and methods
US11015252B2 (en) * 2018-04-27 2021-05-25 Applied Materials, Inc. Protection of components from corrosion
DE102018112353A1 (de) * 2018-05-23 2019-11-28 Forschungszentrum Jülich GmbH Verfahren zur Beschichtung eines Substrates mit einer Hohlraumstruktur
DE102018218018A1 (de) * 2018-10-22 2020-04-23 Siemens Aktiengesellschaft Auftragschweißen von Nickelbasis-Superlegierungen mittels zweier Pulver, Pulvermischung und Verfahren
US10767495B2 (en) 2019-02-01 2020-09-08 Rolls-Royce Plc Turbine vane assembly with cooling feature
US10711621B1 (en) 2019-02-01 2020-07-14 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite components and temperature management features
CN110735117B (zh) * 2019-11-29 2021-06-29 中国航发沈阳黎明航空发动机有限责任公司 一种双联体导向叶片热障涂层制备方法

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US6226978B1 (en) * 1998-04-07 2001-05-08 Ghh Borsig Turbomaschinen Gmbh Hot gas-carrying gas collection pipe of gas turbine
EP1700932A1 (fr) * 2005-03-08 2006-09-13 Siemens Aktiengesellschaft Système de couches avec une couche pour l'inhibition de la diffusion
EP1801263A1 (fr) * 2005-12-21 2007-06-27 United Technologies Corporation Couche de liaison de NiCoCrAly modifié par le platine pour revêtement de barrière thermique
EP1990440A1 (fr) * 2007-04-30 2008-11-12 United Technologies Corporation Revêtement formant barrière thermique multicouche
WO2009038743A1 (fr) * 2007-09-19 2009-03-26 Siemens Energy, Inc. Couche de liaison bimétallique pour un revêtement barrière thermique sur un superalliage
US20110268987A1 (en) * 2009-01-08 2011-11-03 Siemens Aktiengesellschaft Mcralx Layer Having Differing Chromium and Aluminum Content
EP2484799A1 (fr) * 2011-02-02 2012-08-08 United Technologies Corporation Cathode tubulaire segmentée
EP2682488A1 (fr) * 2012-07-05 2014-01-08 Siemens Aktiengesellschaft Système de couche doté d'une couche de protection doble en NiCoCrAIY ayant une teneur en chrome variable et alliage

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Publication number Priority date Publication date Assignee Title
US6226978B1 (en) * 1998-04-07 2001-05-08 Ghh Borsig Turbomaschinen Gmbh Hot gas-carrying gas collection pipe of gas turbine
WO2001023643A2 (fr) * 1999-09-29 2001-04-05 Siemens Westinghouse Power Corporation COUCHE BARRIERE POUR COMBINAISON DE SUPERALLIAGE A COUCHE PRIMAIRE McRAlY
EP1700932A1 (fr) * 2005-03-08 2006-09-13 Siemens Aktiengesellschaft Système de couches avec une couche pour l'inhibition de la diffusion
EP1801263A1 (fr) * 2005-12-21 2007-06-27 United Technologies Corporation Couche de liaison de NiCoCrAly modifié par le platine pour revêtement de barrière thermique
EP1990440A1 (fr) * 2007-04-30 2008-11-12 United Technologies Corporation Revêtement formant barrière thermique multicouche
WO2009038743A1 (fr) * 2007-09-19 2009-03-26 Siemens Energy, Inc. Couche de liaison bimétallique pour un revêtement barrière thermique sur un superalliage
US20110268987A1 (en) * 2009-01-08 2011-11-03 Siemens Aktiengesellschaft Mcralx Layer Having Differing Chromium and Aluminum Content
EP2484799A1 (fr) * 2011-02-02 2012-08-08 United Technologies Corporation Cathode tubulaire segmentée
EP2682488A1 (fr) * 2012-07-05 2014-01-08 Siemens Aktiengesellschaft Système de couche doté d'une couche de protection doble en NiCoCrAIY ayant une teneur en chrome variable et alliage

Also Published As

Publication number Publication date
US20140272456A1 (en) 2014-09-18
EP3372707B1 (fr) 2022-06-29
EP3372707A1 (fr) 2018-09-12
EP4130332A2 (fr) 2023-02-08
US9506140B2 (en) 2016-11-29
EP2971239A1 (fr) 2016-01-20
EP2971239A4 (fr) 2017-03-29
US20160040281A1 (en) 2016-02-11
EP2971239B1 (fr) 2018-05-16
WO2014151788A1 (fr) 2014-09-25
US10113226B2 (en) 2018-10-30

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